Multiple member clad metal products and methods of making the same

ABSTRACT

A new clad metal product free from orange peel effect is provided consisting of a core having at least one layer each of copper and of aluminum coated aluminum alloy and at least one outer cladding layer of stainless steel on the layer of aluminum coated aluminum alloy.

This application is a divisional of my copending application Ser. No. 867,576, filed Jan. 6, 1978 now U.S. Pat. No. 4,167,606, which is in turn a continuation-in-part of my copending application Ser. No. 744,043, now U.S. Pat. No. 4,103,076, filed Nov. 22, 1976 which was in turn a continuation-in-part of my then copending application Ser. No. 572,732, now U.S. Pat. No. 4,004,892, filed Apr. 29, 1975, which was a division of my copending application Ser. No. 423,253, now U.S. Pat. No. 3,952,938, filed Dec. 10, 1973.

This invention relates to multiple member clad metal products and methods of making the same and particularly to a copper core aluminum and stainless steel clad product.

The use of laminated or clad metal products of three laminates or less is well recognized in the industry. For example, stainless steel utensils with a copper bottom layer are well known as are also aluminum cored stainless steels. These products have all been available for some time past and have been extensively used for production of cookware. One of the perennial problems with these prior art materials was and is an inability to get quick and even heat transfer over the entire pan area. These prior art materials are generally far superior to single layer metals but still far from perfect.

My earlier applications of which this application is a continuation-in-part provide a new clad metal product based upon a copper clad aluminum core or a copper core between two layers of aluminum and clad with one or more layers of stainless steel. This new product overcomes the basic problems of the prior art materials discussed above. It will more rapidly and evenly distribute heat. It eliminates the problem of unsightly oxidation of copper in the prior art copper clad stainless steel utensils if used as a core. It provides for superior heat distribution as compared with prior art stainless steel clad aluminum. It combines all the unique thermal properties of copper and aluminum with the corrosion and abrasion resistance properties of stainless steel.

A unique and totally unexpected quality of the metal products of the invention of my earlier applications and of cooking utensils made from the product of those inventions are their property of reducing food adherence to the surface. All metal cooking utensils have been subject to the problem of sticking food stuffs to their surfaces when subject to heat. Teflon and other synthetic coatings have been applied to prevent this in the past. However, the material of this invention is substantially the equal of Teflon coated utensils in preventing sticking.

Note should be made of the excellent heat transfer characteristics of the solid aluminum; copper/aluminum clad stainless; stainless clad aluminum/copper core products, and stainless clad aluminum 2-ply product. Since copper is considered the ultimate in thermal conductivity and is generally considered to be 100%, its ability to transfer heat is well known. Aluminum in its pure state is generally considered to rank second in heat transfer and possesses about 57% that of copper. Cast iron also used for cookware has approximately 16.6% the thermal conductivity of copper whereas carbon steel such as used in the core of stainless clad carbon steel as manufactured by my U.S. Pat. Nos. 2,718,690 and 2,758,368 contains 15.1% of the conductivity of pure copper. Further, stainless steel Type 304 (18% chrome, 8% nickel) has approximately 3.83% the thermal conductivity of pure copper. Ceramic materials similar to glass are total resistors of thermal transfer and have conductivities of approximately 1% that of pure copper.

A direct computation of the percentages of each metal used in the cross section of a clad metal potentially usable for cookware combined with the percentage of thermal conductivity in relation to copper would give one the heat transfer values necessary to determine the thermal conductivity of the as bonded clad metal. The thickness or mass of the metals used in the body of a utensil is also important when considering cooking performance, therefore, we recommend a minimum thickness of 0.050" (1.2 mm.) be used for said application.

Tests were conducted to determine food release characteristics of various materials. Similar sized utensils were placed on top of a gas or electrically heated range containing a center thermocouple capable of touching the exact center of the outside bottom of the utensil. The inside of the utensil was prepared by coating lightly with cooking oil. Flour was then sprinkled on the utensil surface covered with the cooking oil. Excess amounts of flour were removed by gravity throw-off. The resultant thin coating of flour on the surface of the utensil was then observed for color. The utensil was placed on the burner possessing the thermostat and heat was applied by adjusting the burner setting to 350° F. The utensils were subjected to heat for a time element of 21/2 minutes, then were removed from the burner. An attempt to remove the heated flour from the surface of the utensil was made by placing said utensil under a faucet of water at a pressure of 35 lbs. Water temperature of approximately 110° F. was used for rinsing. Time of removal of the flour by the described rinsing process was recorded. The stick resistance was concluded as a direct relation with time of removal of same by said water rinse. The color of the flour is affected by heat concentration. The greater the heat concentration the darker burnt appearance of the flour. Utensil metals with high conductivity produced little or no heat tint on the flour surface. The results, corrected to uniform base of 0.125 thickness, are listed below:

    ______________________________________                                                              Color                                                                          Appearance Removal                                        Product              of Flour   Time                                           ______________________________________                                         1.   Cu/Al/SS (.125 thick)                                                                              Cream      22 secs.                                   2.   Teflon Coated Al (.125 thick)                                                                      Cream      23 secs.                                   3.   Al (.125 thick)     Cream      25 secs.                                   4.   SS Clad Al (.125 thick)                                                                            Cream      29 secs.                                   5.   SS/Al/Cu/Al/SS (.110 thick)                                                                        Cream      33 secs.                                   6.   SS/Al/SS (.110 thick)                                                                              Tan        37 secs.                                   7.   SS Al Bottom (.035 SS/.090 Al)                                                                     Tan-Brown  48 secs.                                   8.   Porcelain coated Steel                                                                             Tan-Brown  39.4 secs.                                      (0.85 thick)                                                              9.   SS Carbon Steel (Iron Core)                                                                        Dark Brown 63.0 secs.                                      (.056 thick)                                                              10.  High temperature glass                                                                             Dark Brown 105 secs.                                  ______________________________________                                    

The food release characteristics of stainless/aluminum/copper utensils were vastly superior to all other metal and glass surfaces. Release characteristics of synthetic surfaces improve with thickness and were equal when 0.125" aluminum thickness was used. Utensils of equal thickness made from copper/aluminum/stainless possessed release characteristics superior to Teflon coated aluminum of equal thickness and utensils of stainless, aluminum copper, aluminum, stainless were in the same range as Teflon coated aluminum. The outstanding thermal properties of the clad metals resulting from the practices taught by this invention are herein described. This characteristic is most important to the establishment of the superiority of the metal combinations herein produced by this invention.

I have discovered that, when pure aluminum alone is used as the cladding for copper, there are instances where an orange peel effect occurs. This orange peeling cannot be controlled by any mechanical or heat treatment known to me. I have discovered, however, that the orange peel effect can be eliminated by using an aluminum alloy base with a thin coating of pure aluminum on the sides to be bonded to the copper and/or stainless steel. This eliminates the problem of orange peeling while giving the very excellent bonding characteristic of pure aluminum. I have found that the base may be an aluminum alloy, e.g. 3003, 3004, 5005 or any other such aluminum product considered by the trade to be an alloy rather than pure aluminum. As the thin pure aluminum coating on the aluminum alloy I may use, for example, EC, 1100, 1130, 1230, 1145, 1175 or 7072 grades of aluminum. This pure aluminum should be clad onto the surfaces of the aluminum alloy which are to be bonded to the copper and stainless steel.

In this specification the word "sheet" or "sheets" is synonymous with coil or sheet coil as used by the metals industry.

In this invention, I accordingly provide an aluminum clad copper in which the aluminum may be clad on one or both sides of the copper. Said aluminum clad copper or copper cored aluminum may then be clad with stainless steel on one or both sides of the aluminum. The aluminum must be substantially pure aluminum, (such as Type 1100, 1130, 1230, 1145, 1175 or 7072) coated on an aluminum alloy such as Type 3003, 3004, 5005. I preferably use an aluminum such as Type 1145 coated as a layer clad on one or both sides of aluminum alloy such as Types 3003, 3004 and 5005. All members of the composite are preferably cleaned and conditioned on their surfaces by abrasive grinding to remove all oxides, however, this can be eliminated for the stainless steel but must be used on the pure aluminum cladding surface of the aluminum alloy. Preferably the product may be made by forming a pre-composite of aluminum and copper, whether the pre-bond be copper clad one side of pure aluminum clad aluminum alloy or aluminum on both sides of a copper core, and thereafter bonding a stainless steel cladding to one or both sides of the aluminum clad aluminum alloy. This pre-formed cladding or core is preferably cleaned and conditioned on the pure aluminum surface or surfaces by abrading or wire brushing or any suitable mechanical method to remove all oxides, however, this can be eliminated for the stainless steel. In this practice the pure aluminum clad aluminum alloy clad copper, or pure aluminum clad aluminum alloy clad copper core has been cleaned as described above, cold bonded under pressure, e.g. by heavy reduction in the level of 40-80% in one or multiple passes on a rolling mill, then post heat treated if desired to increase the strength of the union between same. The pre-formed cladding or core consisting of pure aluminum clad aluminum alloy and copper is heated along with the stainless steel to a temperature of about 300°-800° F., reduced 20-70% in one pass or alternately reduced up to 5% in one roll stand followed by a reduction of 10-25% in a second roll stand, and then reheated to about 600°-800° F., preferably at 700° F. to permit diffusion to occur between the adjacent layers of metals. This diffusion operation causes an increase in the bond strength between the three dissimilar metals, and also causes a certain amount of stress relieving. The resulting product is readily deep drawn into cooking vessels.

As a second alternative, the product may be made by forming a pre-composite cladding or core of pure aluminum clad aluminum alloy and copper and thereafter applying the stainless steel cladding to one or both sides of the pure aluminum surface. In this practice, the pure aluminum clad aluminum alloy and copper sheets are abrasively cleaned and conditioned, brought together into contact, heated to 300°-700° F. and subjected to 30-70% reduction. The pure aluminum clad aluminum alloy and copper composite pre-form may be post heated to increase the strength of the union there between. The resulting copper/aluminum compact is then abrasively cleaned on its pure aluminum surface or surfaces and is used as cladding or core for a stainless cladding operation. In this step the assembly of cladding or core and stainless steel is again heated to about 300°-800° F., subjected preferably to a first reduction of about 2-5%, and then subjected to a second reduction in the range of 5-25%, alternatively the assembly may be reduced in a single reduction pass of about 20-70%. The product is then heat treated to about 700° F. to cause annealing and diffusion as discussed above.

In a third alternative, one or two sheets of pure aluminum clad aluminum alloy are mechanically cleaned, heated to 300°-800° F. and brought into contact with one or both surfaces of a sheet of copper which is at room temperature, and reduced by either the one or two step reductions discussed above. The pre-form composite of pure aluminum clad aluminum alloy and copper may be heat treated if desired to increase the strength of the union between same. This cladding or core is then placed between sheets of stainless steel, reduced and annealed following the practices set forth above.

A fourth alternative would include the manufacture of the pre-form pure aluminum clad aluminum alloy clad on one or both sides of the copper by cold or hot bonding, as discussed in the first alternative, and then the cold bonding of said pre-form of pure aluminum clad aluminum alloy and copper on one or both sides with stainless steel by use of a heavy reduction step at the level of 30-70% in one or two passes. The resulting composite of stainless, copper and aluminum is heat treated as discussed in alternative #1.

In a fifth alternative, all members, i.e., copper, pure aluminum clad aluminum alloy and stainless steel, of the composite are preferably cleaned and conditioned on their exposed surfaces by abrasive grinding to remove all oxides, however, this can be eliminated for the stainless steel. The pieces are heated separately or are brought together prior to heating, heated to a temperature of about 300°-800° F., reduced 20-70% in one pass or alternately reduced up to about 5% in one roll stand followed by a reduction of 10-25% in a second roll stand and then reheated to about 600°-800° F. (preferably at 700° F.) to permit diffusion to occur between the adjacent layers of metal. The diffusion operation causes an increase in bond strength between the three dissimilar metals.

This invention can, perhaps, be best understood by reference to the following examples of products and processes according to this invention and by the accompanying FIGURE showing in section a composite product according to this invention.

EXAMPLE I

A sheet of copper having a thickness of 0.010 inch was abrasively cleaned with a wire brush and placed between two sheets of Type 3003 Aluminum each 0.075 inch thick, coated with a thin layer of Type 1145 Aluminum on both sides which were similarly abrasively cleaned. The copper and the pure aluminum clad aluminum alloy are reduced approximately 50-65% to bond same together. The 0.050 inch thick pre-form of aluminum clad copper was abrasively cleaned on the exposed pure aluminum surface, then brought into contact with two sheets of Type 304 stainless steel 0.010 inch thick, and placed with the stainless steel against the cleaned pure aluminum surfaces. The assembly of metals was heated to 700° F. and passed through a rolling mill to reduce the thickness to 0.065 inch, then passed through a second rolling mill and reduced to a thickness of 0.050 inches. The resulting product was then reheated to 700° F. for a sufficient time to produce diffusion between the adjacent metal layers in their entire interfaces. The final annealed product was deep drawn into cooking vessels such as frypans.

Where it is desired to have one surface of stainless steel and the other of copper, the pre-form consists of a copper clad aluminum material in the same procedures as outlined above are followed but only one side of the copper is clad.

EXAMPLE II

A sheet of 0.010 inch copper was abrasively cleaned and placed between two abrasively cleaned sheets of 0.125 inch Type Alclad 3004 Aluminum coated with Type 1145 Aluminum. The metals were heated to 450° F. and given a first rolling pass at about 2% reduction, and then rolled to about 0.110 inch thickness in a final pass. The rolled product was then reheated to 700° F. to permit diffusion between the metal layers to occur. The final product was cut into blanks and deep drawn into cooking vessels.

Where it is desired to have one surface of stainless steel and the other of aluminum or copper, the same procedures outlined above are followed, omitting the coating which is not to be used.

EXAMPLE III

A sheet of copper having a thickness of 0.010 inch was abrasively cleaned with a wire brush and placed between two sheets of Type 3003 Aluminum alloy each 0.075 inch thick, coated with 1145 Aluminum and similarly abrasively cleaned. Two sheets of Type 304 stainless steel, 0.010 inch thick was abrasively cleaned, was placed on each side of the pure aluminum clad aluminum alloy sheets. The assembly was heated to 700° F. and passed through a rolling mill to reduce the thickness to 0.120 inch. The resulting product was then reheated to 700° F. for a sufficient time to produce diffusion between adjacent metal layers at their interfaces. The final annealed product was deep drawn into cooking vessels.

I have found that the product of this invention can be utilized in the cooking vessel field in a variety of ways and combinations. For example, a nine-ply material shown in the accompanying FIGURE, consisting of a copper core 10 clad on each side with an aluminum alloy sheet 11 coated on each side with pure aluminum 12 which is in turn coated on both sides with stainless steel 13 can be used to form cooking vessels which have the desirable characteristics of stainless steel on the exposed surfaces but have a uniformity of heat transfer unattainable in any prior art materials.

A seven or eight-ply material having a copper core coated on each side with pure aluminum clad aluminum alloy and having one outer layer of stainless is very satisfactory for making cooking vessels which are to be procelainized or coated after forming on the exposed pure aluminum surface or used as discs attached to the bottom of utensils made conventionally from solid or clad metal. Here again the high heat transfer effects are achieved. In such cases where discs are used the coating of pure aluminum on the surface to be exposed is omitted.

Finally, a five-ply material can be made using the procedures outlined above having a copper layer coated on one side with a pure aluminum clad aluminum alloy core and having a copper layer of stainless steel bonded to the pure aluminum surface providing a product which may be formed into cooking utensils having a copper exterior surface for decorative and heat transfer purposes, and the other exterior surface of stainless steel with a core of aluminum.

I have discussed the composition of this invention in this application primarily in terms of cookware because this is the area where the largest amounts of such metals are used, however, the composition of this application can be used in any of a great variety of industrial uses where heat transfer is of importance and where resistance to discoloration, oxidation, etc., are desired.

In the foregoing specification I have set out certain preferred embodiments and practices of my invention, however, it will be understood that this invention may be otherwise embodied within the scope of the following claims. 

I claim:
 1. The method of making a composite clad metal product comprising the steps of first joining together a copper sheet and at least one aluminum alloy sheet coated with substantially pure aluminum on the surfaces to be joined under pressure sufficient to provide a reduction up to 80%, post-heat treating the same, mechanically cleaning the aluminum surface, placing said mechanically cleaned pre-bonded aluminum-copper composite on at least one sheet of stainless steel with the aluminum adjacent to the stainless steel, heating the stacked metals to a temperature between 300° F. to 800° F. and subjecting the stacked metals to sufficient pressure to a first reduction of about 2% followed by a reduction of about 5 to 25%.
 2. A method of making a composite metal product comprising assembling a copper sheet, at least one aluminum sheet coated with substantially pure aluminum on the surfaces to be joined and at least one stainless steel sheet with the aluminum sheet between the copper and stainless steel sheets, heating said metal sheets to a temperature between 300° F. to 800° F. and then joining the assembled heated sheets under pressure sufficient to produce a reduction of about 20 to 70%.
 3. The method as claimed in claim 1 or 2 wherein the sheets being joined consist of a copper sheet, a pair of aluminum alloy sheets coated with substantially pure aluminum on each surface, one of said pair of aluminum alloy sheets on each opposite surface of the copper sheet and a stainless steel sheet on at least one surface of the aluminum opposite the copper.
 4. A method as claimed in claim 1 or 2 wherein the pre-bonded aluminum-copper composite and the stainless steel sheet are heated in separate furnaces and then stacked one on the other.
 5. A method as claimed in claim 1 or 2 wherein the sheets are joined by passing through a rolling mill.
 6. A method as claimed in claim 1 or 2 wherein the sheets are post heat-treated up to about 700° F. following the last reduction.
 7. A method as claimed in claim 3 wherein the sheets are joined by passing through a rolling mill.
 8. A method as claimed in claim 3 wherein the sheets are post heat-treated to about 700° F. following the last reduction.
 9. The method of making a composite clad metal product comprising first joining together a copper sheet and at least one aluminum alloy sheet coated with substantially pure aluminum on the surfaces to be joined under pressure sufficient to provide a reduction up to 80%, post-heat treating same, mechanically cleaning the aluminum surface, placing said mechanically cleaned pre-bonded composite on at least one sheet of stainless steel, subjecting the stacked metals to a first reduction of about 2% followed by a reduction of about 5 to 25%.
 10. The method of making a composite product comprising cleaning a copper sheet, at least one aluminum sheet coated with substantially pure aluminum on the surfaces to be joined and at least one stainless steel sheet to be joined including mechanical cleaning of said aluminum surfaces to be joined, assembling said sheets with the aluminum sheet between the copper and stainless steel sheets and joining the assembled sheets under pressure sufficient to produce a reduction of about 20% to 70%.
 11. The method as claimed in claim 9 or 10 wherein the sheets being joined consists of a copper sheet, a pair of aluminum alloy sheets coated with substantially pure aluminum on each surface, one of said pair of aluminum alloy sheets on each opposite surface of the copper sheet and a stainless steel sheet of stainless steel on at least one surface of the aluminum opposite the copper.
 12. A method as claimed in claim 9 or 10 wherein the sheets are joined by passing through a rolling mill.
 13. A method as claimed in claim 9 or 10 wherein the sheets are post-heat treated at about 700° F. following the last reduction.
 14. The method of making a composite clad metal product comprising the steps of first heating a copper sheet and at least one aluminum alloy sheet coated with substantially pure aluminum on the surfaces to be joined to a temperature between 300° F. to 800° F., then joining said heated sheets together under pressure sufficient to provide a reduction of 20 to 70%, post heat-treating same, mechanically cleaning the aluminum surface, placing said mechanically cleaned pre-bonded composite on at least one sheet of stainless steel with the stainless steel in contact with the cleaned aluminum surface, heating the stacked metals to a temperature between 300° F. to 800° F., and subjecting the stacked metals to sufficient pressure to a first reduction of about 2% followed by a reduction of about 5 to 25%.
 15. The method as claimed in claim 14 wherein the sheets being joined consists of a copper sheet, a pair of aluminum alloy sheets coated with substantially pure aluminum on each surface, one of said pair of aluminum alloy sheets on each opposite surface of the copper sheet and a stainless steel sheet on at least one surface of the aluminum opposite the copper.
 16. A method as claimed in claim 14 wherein the pre-bonded aluminum-copper composite and the sheet of stainless steel are heated in separate furnaces and then stacked one on the other.
 17. A method as claimed in claim 14 wherein the sheets are joined by passing through a rolling mill.
 18. A method as claimed in claim 15 wherein the sheets are post heat-treated to about 700° F. following the last reduction.
 19. The method of making a composite clad metal product comprising the steps of first heating a copper sheet and at least one aluminum alloy sheet coated with substantially pure aluminum on the surfaces to be joined to to a temperature between 300° F. to 800° F. then joining said heated sheets together under pressure sufficient to provide a reduction of 20 to 70%, postheat treating same, mechanically cleaning the aluminum surface, placing said mechanically cleaned pre-bonded composite on at least one sheet of stainless steel with the stainless steel in contact with the cleaned aluminum surface, subjecting the stacked metals to a first reduction of about 2% followed by a reduction of about 5 to 25%.
 20. The method of making a composite clad metal product wherein a copper sheet, at least one aluminum sheet coated with substantially pure aluminum on the surfaces to be joined and at least one stainless steel sheet are first heated to to a temperature between 300° F. to 800° F., then assembled with the aluminum sheet between the copper and the stainless steel sheets, the assembled sheets are joined under pressure sufficient to produce a reduction of about 20 to 70% and the product is post heat treated.
 21. The method as claimed in claim 19 or 20 wherein the sheets being joined consist of a copper sheet, a pair of aluminum alloy sheets coated with substantially pure aluminum on each surface, one of said pair of aluminum alloy sheets on each opposite surface of the copper sheet and a stainless steel sheet on at least one surface of the aluminum opposite the copper.
 22. A method as claimed in claim 19 or 20 wherein the metal sheets are heated in separate furnaces.
 23. A method as claimed in claim 19 or 20 wherein the sheets are joined by passing through a rolling mill.
 24. A method as claimed in claim 22 wherein the sheets are post-heat treated up to about 700° F. following the last reduction.
 25. The method of making a clad metal product characterized by a high rate of thermal transmission and by resistance to corrosion comprising the steps of:a. mechanically cleaning the surfaces of each of a sheet from the group consisting of copper and copper alloys, and at least one aluminum alloy sheet coated with substantially pure aluminum; b. placing said mechanically cleaned sheets one on top of the other and applying at least one sheet of stainless steel on the aluminum; c. heating said sheets to a temperature of about 300° F. to 800° F.; d. joining said sheets under pressure sufficient to reduce the total thickness of said sheets an approximately 2% in the first reduction step and between 5 and 25% reduction in the second reduction step; e. stress relieving the joined sheets at a temperature of about 700° F.
 26. The method of making a clad metal product characterized by a high rate of thermal transmission and by resistance to corrosion comprising the steps of:(a). mechanically cleaning the surfaces of each of a sheet from the group consisting of copper and copper alloys, and at least one aluminum alloy sheet coated with substantially pure aluminum; (b). placing said mechanically cleaned sheets one on top of the other and applying sufficient pressure to join the sheets to form a pre-bonded composite; (c). applying at least one sheet of stainless steel on the aluminum; (d). heating said sheets to a temperature of about 300° F. to 800° F.; (e). joining said sheets under pressure sufficient to reduce the total thickness of said sheets approximately 2% in a first reduction step and between 5% and 25% reduction in a second reduction step; and (f). stress relieving the joined sheets at a temperature of about 700° F.
 27. The method of making a composite clad metal product comprising the steps of first joining together a copper sheet and at least one aluminum alloy sheet coated with substantially pure aluminum on the surfaces to be joined under pressure sufficient to provide a reduction up to 80%, post-heat treating the same, mechanically cleaning the aluminum surface, placing said mechanically cleaned pre-bonded aluminum-copper composite on at least one sheet of stainless steel with the aluminum adjacent to the stainless steel, heating the stacked metals to a temperature between 300° F. to 800° F. and subjecting the stacked heated metals to sufficient pressure to produce a reduction of about 20% to 70%.
 28. The method of making a composite clad metal product comprising the steps of first joining together a copper sheet and at least one aluminum alloy sheet coated with substantially pure aluminum on the surfaces to be joined under pressure sufficient to provide a reduction up to 80%, post-heat treating same, cooling, mechanically cleaning the aluminum surface, placing said mechanically cleaned pre-bonded composite on at least one sheet of stainless steel, subjecting the stacked metals to a pressure sufficient to produce a reduction of about 20% to 70%.
 29. The method of making a composite clad metal product comprising first heating a copper sheet and at least one aluminum alloy sheet coated with substantially pure aluminum on the surfaces to be joined to a temperature between 300° F. to 800° F., then joining said heated sheets together under pressure sufficient to provide a reduction of 20 to 70%, post-heat treating same, mechanically cleaning the aluminum surface, placing said mechanically cleaned pre-bonded composite on at least one sheet of stainless steel, heating the stacked metals to a temperature between 300° F. to 800° F., and subjecting the stacked metals to sufficient pressure to produce a reduction of about 20% to 70%.
 30. The method of making a composite clad metal product comprising the steps of first heating a copper sheet and at least one aluminum alloy sheet coated with substantially pure aluminum on the surfaces to be joined to to a temperature between 300° F. to 800° F. then joining said heated sheets together under pressure sufficient to provide a reduction of 20 to 70%, post-heat treating same, mechanically cleaning the aluminum surface, placing said mechanically cleaned prebonded composite on at least one sheet of stainless steel, subjecting the stacked metals to a pressure sufficient to produce a reduction of about 20% to 70%.
 31. The method as claimed in claim 25 or 26 wherein the sheets are joined by passing through a rolling mill.
 32. A method as claimed in claim 26 wherein the pre-bonded aluminum-copper composite and the stainless steel sheet are heated in separate furnaces and then stacked one on the other.
 33. A method as claimed in claim 26, or 27, or 28, or 29 wherein the sheets being joined consist of a copper sheet, a pair of aluminum alloy sheets coated with substantially pure aluminum on each surface, one of said pair of aluminum alloy sheets on each opposite surface of the copper sheet and a stainless steel sheet on at least one surface of the preformed copper/aluminum core.
 34. A method as claimed in claim 27, or 28, or 29, or 30 wherein the sheets are joined by passing through a rolling mill.
 35. A method as claimed in claim 27, or 28, or 29, or 30 wherein the sheets are post-heat treated up to about 700° F. following the last reduction.
 36. A method as claimed in claim 25, or 27, or 28, or 29, or 30 wherein the sheets are heated in separate furnaces and then stacked one on the other.
 37. A method of making a composite clad metal product comprising the steps of first joining together a copper sheet and at least one aluminum alloy sheet coated with substantially pure aluminum on the surfaces to be joined under a pressure sufficient to provide a reduction of about 80%, post-heat treating the bonded aluminum copper composite, heating the pre-bonded aluminum copper composite to a temperature in the range 300° F. to 800° F., placing said heated aluminum-copper composite on at least one sheet of stainless steel with the aluminum abutting the stainless steel and subjecting the stacked metals to sufficient pressure to produce a first reduction of about 2% followed by a reduction of about 5% to 25%.
 38. A method of making a composite clad metal product comprising the steps of first joining together a copper sheet and at least one aluminum alloy sheet coated with substantially pure aluminum on the surfaces to be joined under a pressure sufficient to provide a reduction of about 80%, post-heat treating the bonded aluminum copper composite, heating the pre-bonded aluminum-copper composite to a temperature in the range 300° F. to 800° F., placing the heated composite on at least one sheet of stainless steel with the aluminum abutting the stainless steel and subjecting the stacked metals to sufficient pressure to produce a reduction of about 20% to 70%.
 39. A method as claimed in claim 37 or 38 wherein the sheets being joined consist of a copper sheet, a pair of aluminum alloy sheets coated with substantially pure aluminum on each surface, one of said pair of aluminum alloy sheets on each opposite surface of the copper sheet and a stainless steel sheet on at least one surface of the preformed copper/aluminum core.
 40. A method as claimed in claim 37 or 38 wherein the sheets are joined by passing through a rolling mill.
 41. A method as claimed in claim 37 or 38 wherein the sheets are post-heat treated up to about 700° F. following the last reduction.
 42. A method as claimed in claim 37 or 38 wherein the sheets are heated in separate furnaces and then stacked one on the other. 